Cessna 152 - Page 76

I
THIS DATA APPLICABLE ONLY TO AIRPLANES WITH LYCOMING
0-235--UC ENGINE.
FOR
AIRPLANES WITH ENGINE MODIFIED TO
0-235--N2C.
REFER
TO DATA
IN
SECTION 9 SUPPLEMENT.
SECTIONS
PERFORMANCE
CONDITIONS:
1670
Pounds
CRUISE
PERFORMANCE
Recommended Lean Mixture (See Section
4,
Cruise)
NOTE:
CESSNA
MODEL
152
Cruise speeds are shown for an airplane equipped with
speed
fairings which increase
the
speeds
by approximately
two
knots.
PRESSURE
ALTITUDE
RPM
FT
2000
2400
2300
2200
2100
2000
4000
2450
2400
2300
2200
2100
2000
6000
2500
2400
2300
2200
2100
2000
8000
2550
2500
2400
2300
2200
2100
10,000
2500
2400
2300
2200
2100
12,000
2450
2400
2300
2200
2100
5-14
20°c
BELOW
STANDARD
20°C ABOVE
STANDARD TEMP TEMPERATURE
STANDARD TEMP
%
% %
KTAS
GPH
KTAS
GPH
KTAS
GPH
BHP
BHP BHP
-
-
-
--
-
-
--
75
101
6.1
70
101
5.7
71
97
5.7
66
.9,6
5.4
63
95
5.1
62
92
5.1
59
91
4.8
56
90
4.6
55 87
4.5
53
86 4.3
51
85
4.2
49
81
4.1
47
80
3.9
46
79 3.8
- - -
-
-
-
-
- -
75
103
6.1
70 102 5.7
76
102
6.1
71
101
6.7
67 100 5.4
67
96
5.4
63
95
5.1
60
95
4.9
60
91
4.8
56
90
4.6
54
89
4.4
53
86
4.4
51
85
4.2
49
84
4.0
48
81
3.9
46
80
3.8
45
78 3.7
-
-
- - - -
-
-
-
75
105 6.1
71
104 5.7
72
101
5.8
67
1.00
5.4
64
99
5.2
64
96
5.2
60
96
4.9
57
94
4.7
57
90
4.6
54
89
4.4
52
88 4.3
51
85
4.2
49
84
4.0
48
83
3.9
46
80
3.8
45
79 3.7
44
77
3.6
-
- -
- - -
-
-
-
75
107
6.1
71
106 5.7
76
105
6.2
71
104 5.8
67 103
5.4
68
100
5.5
64
99
5.2
61
98
4.9
61
95
5.0
58
94
4.7
55
93
4.5
55
90
4.5
52
89
4.3
51
87 4.2
49
84
4.1
48
83 3.9
46
82
3.8
72
105
5.8
68 103 5.5
64
103 5.2
65
99
5.3
61
98
5.0
58
97
4.8
58
94
4.7
56
93
4.5
53
92
4.4
53
89
4.3
51
88
4.2
49
86 4.0
48
83
4.0
46
82
3.9
45
81
3.8
65
101
5.3
62
100 5.0
59
99 4.8
62
99
5.0
59
97
4.8
56
96
4.6
56
93
4.6
54
92
4.4
52
91
4.3
51
88
4.2
49
87
4.1
48
85
4.0
47
82
3.9
45
81
3.8
44
79 3.7
Figure
5-7.
Cruise
Performance
1
July
1978
Revision
1 -
31
March
1983